GB2422895A - An assembly for incorporation within a turret providing access to a cryostat - Google Patents
An assembly for incorporation within a turret providing access to a cryostat Download PDFInfo
- Publication number
- GB2422895A GB2422895A GB0502457A GB0502457A GB2422895A GB 2422895 A GB2422895 A GB 2422895A GB 0502457 A GB0502457 A GB 0502457A GB 0502457 A GB0502457 A GB 0502457A GB 2422895 A GB2422895 A GB 2422895A
- Authority
- GB
- United Kingdom
- Prior art keywords
- positive tube
- thermal
- thermal link
- tube
- turret
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000010348 incorporation Methods 0.000 title claims abstract description 4
- 239000000853 adhesive Substances 0.000 claims abstract description 26
- 230000001070 adhesive effect Effects 0.000 claims abstract description 26
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims abstract description 17
- 239000003822 epoxy resin Substances 0.000 claims abstract description 13
- 229920000647 polyepoxide Polymers 0.000 claims abstract description 13
- 239000002245 particle Substances 0.000 claims abstract 2
- 238000000034 method Methods 0.000 claims description 13
- 239000010410 layer Substances 0.000 claims description 9
- 239000000945 filler Substances 0.000 claims description 5
- 239000007788 liquid Substances 0.000 claims description 5
- 239000012790 adhesive layer Substances 0.000 claims description 2
- 230000013011 mating Effects 0.000 claims 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 abstract description 8
- 229910052802 copper Inorganic materials 0.000 abstract description 8
- 239000010949 copper Substances 0.000 abstract description 8
- 229910001220 stainless steel Inorganic materials 0.000 abstract description 8
- 239000010935 stainless steel Substances 0.000 abstract description 8
- 239000004020 conductor Substances 0.000 abstract description 3
- 238000002955 isolation Methods 0.000 description 7
- 238000002595 magnetic resonance imaging Methods 0.000 description 6
- 230000004907 flux Effects 0.000 description 5
- 239000000463 material Substances 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 239000003054 catalyst Substances 0.000 description 3
- 230000004941 influx Effects 0.000 description 3
- 230000015556 catabolic process Effects 0.000 description 2
- 238000007750 plasma spraying Methods 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 229910000679 solder Inorganic materials 0.000 description 2
- 238000005476 soldering Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229920002472 Starch Polymers 0.000 description 1
- 230000002745 absorbent Effects 0.000 description 1
- 239000002250 absorbent Substances 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 238000009529 body temperature measurement Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 239000011247 coating layer Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000008107 starch Substances 0.000 description 1
- 235000019698 starch Nutrition 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/005—Details of vessels or of the filling or discharging of vessels for medium-size and small storage vessels not under pressure
- F17C13/006—Details of vessels or of the filling or discharging of vessels for medium-size and small storage vessels not under pressure for Dewar vessels or cryostats
- F17C13/007—Details of vessels or of the filling or discharging of vessels for medium-size and small storage vessels not under pressure for Dewar vessels or cryostats used for superconducting phenomena
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F6/00—Superconducting magnets; Superconducting coils
- H01F6/04—Cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/08—Mounting arrangements for vessels
- F17C13/086—Mounting arrangements for vessels for Dewar vessels or cryostats
- F17C13/087—Mounting arrangements for vessels for Dewar vessels or cryostats used for superconducting phenomena
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D19/00—Arrangement or mounting of refrigeration units with respect to devices or objects to be refrigerated, e.g. infrared detectors
- F25D19/006—Thermal coupling structure or interface
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/05—Applications for industrial use
- F17C2270/0527—Superconductors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Containers, Films, And Cooling For Superconductive Devices (AREA)
Abstract
An assembly for incorporation within a turret 12 providing access to a cryogen vessel of a cryostat comprises a positive tube 10 which acts as an electrical conductor for introducing electrical current into equipment within the cryogen vessel. The tube 10 may be of thin-walled stainless steel. The equipment may be, for example, a superconducting magnetic coil of an MRI system. A thermal intercept 16, cooled by a refrigerator, is provided in thermal contact with the turret 12. A thermal link 18 joins the interior surface of the turret 12 to the exterior surface of the positive tube 10. The thermal link 18 and the thermal intercept 16 are preferably a single copper block with separate sections of the turret 12 bonded into suitably shaped channels within the thermal intercept 16. A thermally conductive, but electrically isolating mechanical joint 20 is made between the positive tube 10 and the thermal link 18 using an adhesive such as epoxy resin. When cured the epoxy resin may contain particles of alumina.
Description
TURRET THERMAL INTERCEPT JOINT
Fig. 1 shows a cryostat such as may be employed for holding magnet coils for an MRI (magnetic resonance imaging) system. A cryogen vessel I holds a liquid cryogen 2.
The space 3 in the cryogenic vessel above the level of the liquid cryogen may be filled with evaporated cryogen. The cryogen vessel is contained in a vacuum jacket 4 which serves to reduce the amount of heat flowing to the cryogen 2 from ambient temperature, by reducing the possibility of conduction or convection heating of the cryogen vessel I. One or more heat shields 5 may be provided in the vacuum space between the cryogen vessel I and the vacuum jacket 4. These shields serve to reduce the amount of radiated heat reaching the cryogen vessel 1 from the exterior. An access neck 6 is provided, allowing access to the cryogenic vessel from the exterior. This is used to fill the cryogen vessel, to provide access for current leads and other connections to superconductive coils housed within the cryogen vessel, and to allow an escape path for boiled- off gaseous cryogen.
A positive tube 10, typically a thin walled stainless steel tube, passes into the cryogen vessel. An electrical lead 9 connects the positive tube to equipment, such as superconducting coils (not shown) for NMR or MRI magnets. The positive tube 10 is also connectable to a current source external to the cryostat, for introducing electrical current into equipment within the cryogen. The positive tube 10 is typically connected to the positive terminal of the current source, with the negative current return path being provided through the structure of the cryostat. Since the positive tube 10 extends through the access neck 6, from the cryogen vessel I to the exterior, it provides a path for heat influx into the cryogen vessel. This problem is typically addressed by thermally linking the positive tube 10 to a cooled part, such as the thermal shield 5. In the illustrated cryostat, this is achieved by providing a thermal link I 8, through which the positive tube passes, in thermal connection but electrical isolation. A passageway is provided in the thermal link 1 8 to provide access for other connections, for cryogen lill and to allow gaseous cryogen to escape in the event of a quench. Th
The positive tube 10 is typically housed within a turret 12, typically another thin walled stainless steel tube. A lower part olturret 12 may itself be housed within a bellows 14.
In position, the bellows forms part of the cryogen vessel I. The bellows 14 is typically a thin walled stainless steel tube of greater diameter than the positive tube 10 and the turret 12. The bellows accommodates a length of the turret 12 and the positive tube 10 extending down into the cryogen vessel 1. The extended length of the turret 12 and the positive tube 10 allowed by the bellows 14 increases their thermal path length and so helps to reduce thermal influx into the cryogen vessel. The bellows structure serves to accommodate differences in thermal expansion and other relative movement between the cryogen vessel 1, the thermal shield 5 and the outer vacuum chamber 4.
Fig. 2 illustrates a fixed positive tube access neck 6 according to the prior art. A positive tube 10, typically comprising a thin-walled stainless steel tube, acts as an electrical conductor for introducing electrical current into equipment within the cryogen vessel I. Such equipment may typically be superconducting magnetic coils for an MRI system. The positive tube must be insulated from other electrically conductive components since the return path for the current is generally through the structure of the cryostat.
It is desired that the positive tube 10 be cooled by a refrigerator, typically to a temperature of the order of 50K. This serves to reduce the heat influx into the cryogen vessel I, by removing heat flowing from ambient along the material of the positive tube before it reaches the cryogen vessel I. As shown in Fig. 2, a thermal intercept 16 is provided, mechanically and thermally in contact with the turret 12. In a preferred embodiment, separate sections of turret 12 are bonded into suitably shaped channels within the thermal intercept 16, so that a single piece of thermally conductive material, typically copper, extends from the exterior of the turret 12 to its interior. I'his thermal intercept I 6 is cooled by thermal conduction along a conductive path to a refrigerator. The refrigerator in question is typically the first stage of a two-stage recondensing refrigerator, which cools the thermal intercept 16 to approximately 50K.
In order to provide the required thermal cooling and electrical isolation for the positive tube 10, a thermal link I 8 is provided, joining the interior surface of the turret 12 to the exterior surface of the positive tube 10. Thermal link 18 and thermal intercept 16 are typically a single copper block, with separate sections of turret 12 bonded into suitably shaped channels within the thermal intercept 16. Thermal link 18, in such an embodiment, simply refers to that part of the thermal intercept which is located within the turret 12. Thermal link 18 must also provide electrical isolation between the positive tube 10 and the turret 12. The thermal link 18 preferably also provides mechanical support to the positive tube 10. The thermal link is cooled, through the material of the turret 12, by thermal conduction to thermal intercept 16.
According to the prior art, these requirements have been met by the following process.
The positive tube 10, typically a stainless steel tube, is plasma sprayed with alumina, at least in a band around the tube in a region destined to contact the thermal link 18. The positive tube is then plasma sprayed with copper over at least part of the region which has been sprayed by alumina, at least in a band around the tube in a region destined to contact the thermal link 18. The resultant structure will then comprise, at least in a band around the tube in a region destined to contact the thermal link 1 8, a stainless steel tube coated in an electrically insulating layer of alumina, which in turn is coated in an electrically conductive layer of copper. The layers are strongly mechanically linked, and have thermal conductivity. The stainless steel of the positive tube 10 and the copper coating layer are however electrically isolated.
The thermal link 18 typically has an inner diameter slightly greater than the outer diameter of the copper and alumina coated positive tube. Although not clearly visible in Fig. 2, a kidney-shaped passage is provided through the thermal link 18 to allow the passage of other services, cryogen fill and escape of cryogen gas in the case of a quench.
The thermal link 18 is slid over the positive tube 10 to the appropriate position. The thermal link 18 and the positive tube 10 are then heated, at least in the appropriate regions, sufficiently to allow soft soldering of the joint between them. The thermal link 18 is soft soldered to the copper coating on the positive tube. The resultant electrical isolation has been measured at under I 0M = at I OOV.
This method has at least the following drawbacks. The plasma spraying processes are difficult and costly to perform. The alumina used lbr plasma spraying, and the resultant alumina layer on the positive tube, is moisture absorbent and so requires careful drying, handling and storage. Moisture in the alumina can cause electrical breakdown, leading to an electrical short circuit between the positive tube and the structure of the cryostat, which can render the part useless since it will no longer be possible to supply current to the equipment inside the cryogen vessel 1. For soldering, it is necessary to heat the thermal joint and the positive tube to beyond the melting point of the solder. This is a time consuming step and requires appropriate process equipment. Before solder is applied, a flux must be applied to clean and prepare the surfaces of the positive tube and the thermal link. The chemistry of the flux means that it may damage surrounding metals. Any residue left by the flux is typically washed off with water, wetting the alumina layer which must then be carefully dried.
The present invention accordingly aims to address at least some of the drawbacks of the prior art, while producing a structure which provides sufficient electrical, thermal and mechanical performance.
The above, and further, objects, characteristics and advantages of the present invention will become more apparent from the following description of certain embodiments thereof, given by way of examples only, in conjunction with the appended drawings, wherein: Th Fig. 1 shows a cross-section of a typical cryostat, such as may be used to house superconducting magnets in MRI applications, and which could benefit from application of the present invention; Fig. 2 shows a positive tube housed within a turret and thermally connected to a
thermal intercept, according to the prior art; and
Fig. 3 shows a positive tube housed within a turret and thermally connected to a thermal intercept, according to an embodiment of the present invention.
Fig. 3 illustrates an enlarged detail of a fixed positive tube service turret according to an embodiment of the present invention. The part illustrated in Fig. 3 corresponds to the region III outlined in Fig. 2.
According to the present invention, the thermal link 18 is not soldered to the positive tube 10. Rather, according to the present invention, a thermally conductive yet electrically isolating mechanical joint 20 is made between the positive tube 10 and the thermal link 18 using an adhesive such as an epoxy resin. The adhesive in question must be thermally conductive, but electrically isolating.
In certain embodiments of the invention, the adhesive used is ECCOBOND 285 epoxy resin or STYCAST 2850FT epoxy resin, both available from Emerson & Cuming, 46 Manning Road, Billerica MA, USA. The epoxy resin may be caused to harden by incorporation of Catalyst 9, or Catalyst 11, each available from Emerson & Cuming. The epoxy resin used is preferably filled with a highly thermally conductive, yet electrically isolating, filler. In certain embodiments, the filler may be a fine grained alumina (Al203) powder.
The combination o ECCOBOND 285 epoxy resin with Catalyst 9 is known to provide a thermal conductivity of 1.3 W m1 K', and a volume resistivity of 10N cm at a temperature of about 300K. Another useful property of ECCOBOND 285 epoxy resin in this application is its relatively low coefficient of thermal expansion, quoted by n the manufacturer as 106 K1. Such epoxy resin adhesives have been found by the inventors to be tolerant of operating at temperatures of around 50K, as required for use in the present application in MRI systems cooled by liquid helium cryogen.
In alternative embodiments, adhesives other than epoxy resins may be used. For example, silicone or polyurethane adhesives may be used, preferably with thermally conductive but electrically isolating fillers such as alumina powder. Whatever adhesive is used, it must have the required properties of high thermal conductivity, high electrical resistance and tolerance of temperatures in the region of interest, for example about 50K.
ECCOBOND and STYCAST are registered trademarks of the National Starch and Chemical Company.
In order to form the adhesive joint 20 of the present invention between the positive tube and the thermal link I 8, the following method may be employed.
A quantity of the selected adhesive is applied around the positive tube 10, covering at least a band around the positive tube in a location where the joint 20 to the thermal link will be made. The thermal link 18 is then slid over the positive tube to the appropriate position. The adhesive will be squeezed between the outer surface of the positive tube and the inner surface of the thermal link. It has been found that the adhesive effectively coats both of these surfaces. Any excess adhesive may be cleaned in a normal manner, such as by wiping with a cloth, if necessary. It may be found more effective to rotate the thermal link about the positive tube as it slides over the adhesive layer. This may assist the centring of the positive tube 10 within the thermal link 18.
This process may be carried out at normal room temperature.
K
Since the adhesive is conformal to the surfaces being joined, the joint 20 according to the present invention is tolerant of a larger degree of deformation of the positive tube than is the case for the soldered joint of the prior art.
There is no need to apply a flux to the surfaces to he joined in the method of the present invention, avoiding the possibility of chemical damage to surrounding materials by such flux. There is no need to heat the positive tube and thermal link, as there was in
the case of the soldered joint of the prior art.
The cost of forming the adhesive joint 20 between the positive tube 10 and the thermal link 18 according to the present invention is only about 10-20% of the cost of forming
the soldered joint of the prior art.
The adhesives used to form the joint 20 according to the present invention do not absorb water to a significant degree. A moisture absorption of 0.1% after 24 hours at a temperature of 300K is typical. Alumina, on the other hand, may absorb up to 50% moisture, and a corresponding figure for dried' alumina would be in the region of 10%.
The resultant electrical isolation provided by the joint 20 of the present invention between the positive tube and the thermal link has been measured at over l5OMf = at 250V, which compares very favourably with the isolation of the soldered joint of the prior art, which had an electrical isolation measured at under I 0M1 at I OOV.
The thermal conductivity of the joint 20 of the present invention may be less than that of the soldered joint of the prior art. For example, a joint 20 of the present invention using STYCAST 258FT has been measured to have a thermal conductivity of 0.46 Wm1K', whereas a joint according to the prior art has been measured to have a thermal conductivity of 2.6WrnK* The effect of this reduced thermal conductivity is expected to he a temperature rise of approximately 1K in the region of the joint 20.
The inventors regard this degree of degradation of thermal conductivity as an acceptable price to pay for the other advantages offered by the joint 20 of the present invention. The inventors expect that further investigation by routine trial and error or another methods will identily filled adhesive materials which provide better thermal performance. The cited example of STYCAST 258FT alumina-filled epoxy resin adhesive has previously been used in cryogenic applications, for example for attaching temperature measurement equipment into cryostats. It is accordingly known that such adhesive is reliable at the temperatures under consideration in the present application.
While the present application has been described with reference to a limited number of specific embodiments, various amendments and modifications may be made within the scope of the present invention as defined by the appended claims.
Claims (9)
- CLAIMS: 1. An assembly for incorporation within a turret (12) providingaccess to a cryogen vessel (I) of a cryostat, the assembly comprising: - a positive tube (JO); and - a thermal link (18) mechanically bonded to the positive tube by a thermally conductive, electrically isolating joint (20), characterised in that the joint (20) is formed by a layer of adhesive formed between respective mating surlces of the positive tube and the thermal link.
- 2. An assembly according to claim I wherein the adhesive comprises a cured epoxy resin containing thermally conductive, electrically isolating filler.
- 3. An assembly according to claim 2 wherein the filler comprises particles of alumina Al203.
- 4. An assembly according to any preceding claim, wherein the positive tube is substantially cylindrical, and the thermal link is annular, bonded around a part of the outer surface of the tube.
- 5. A cryostat comprising a cryogen vessel (1) for containing a liquid cryogen (2) and a two-stage refrigerator for recondensing gaseous cryogen boiled off from the liquid cryogen, a turret (12) providing access to the cryogen vessel and housing an assembly according to any of claims 1-4, wherein a first stage of the two stage refrigerator is thermally connected to the thermal link (18).
- 6. A method for assembling a positive tube (JO) into a turret (12) in such a manner that the positive tube is mechanically and thermally connected but electrically isolated from the turret by a thermal link (18) , the method comprising the step of - bonding the thermal link to a part of an outer surface of the positive tube by way of a layer of adhesive. - 10-
- 7. A method according to claim 6, wherein the step of bonding the thermal link to a part of an outer surface of the positive tube by way of a layer of adhesive itself comprises the steps of: - applying a layer of adhesive around the positive tube (10), to cover at least a band around the positive tube in a location where the bond to the thermal link will be made; - sliding the thermal link (18) over the positive tube to the appropriate position, whereupon the adhesive will be squeezed between the outer surface of the positive tube and the inner surface of the thermal link; and - curing the adhesive.
- 8. A method according to claim 7 wherein the positive tube is substantially cylindrical and the thermal link is substantially annular and the thermal link is rotated about the positive tube as it slides over the adhesive layer.
- 9. An assembly, cryostat or method substantially as described.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB0502457A GB2422895B (en) | 2005-02-05 | 2005-02-05 | An Assembly Providing a Tubular Electrical Conductor in Thermal Contact but Electrical Isolation with a Thermal Link |
| CN2006100043784A CN1816270B (en) | 2005-02-05 | 2006-01-27 | An assembly that provides a tubular conductor that is in thermal contact with, but electrically insulated from, a thermal connection |
| US11/346,342 US20060207266A1 (en) | 2005-02-05 | 2006-02-03 | Assembly providing a tubular electrical conductor in thermal contact but electrical isolation with a thermal link |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB0502457A GB2422895B (en) | 2005-02-05 | 2005-02-05 | An Assembly Providing a Tubular Electrical Conductor in Thermal Contact but Electrical Isolation with a Thermal Link |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB0502457D0 GB0502457D0 (en) | 2005-03-16 |
| GB2422895A true GB2422895A (en) | 2006-08-09 |
| GB2422895B GB2422895B (en) | 2007-08-01 |
Family
ID=34355886
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB0502457A Expired - Lifetime GB2422895B (en) | 2005-02-05 | 2005-02-05 | An Assembly Providing a Tubular Electrical Conductor in Thermal Contact but Electrical Isolation with a Thermal Link |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20060207266A1 (en) |
| CN (1) | CN1816270B (en) |
| GB (1) | GB2422895B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2456571A (en) * | 2008-01-21 | 2009-07-22 | Siemens Magnet Technology Ltd | Power Supply Coupling System |
| GB2513151A (en) * | 2013-04-17 | 2014-10-22 | Siemens Plc | Improved thermal contact between cryogenic refrigerators and cooled components |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2462626B (en) * | 2008-08-14 | 2010-12-29 | Siemens Magnet Technology Ltd | Cooled current leads for cooled equipment |
| US9640308B2 (en) * | 2008-10-14 | 2017-05-02 | General Electric Company | High temperature superconducting magnet |
| US8415952B2 (en) | 2009-12-23 | 2013-04-09 | General Electric Company | Superconducting magnet coil interface and method providing coil stability |
| CN104143405B (en) * | 2013-05-10 | 2018-08-31 | 上海联影医疗科技有限公司 | A kind of connection structure and its manufacturing method |
| CN204177947U (en) * | 2014-10-16 | 2015-02-25 | 西门子(深圳)磁共振有限公司 | Gas outlet, superconducting magnet and MR imaging apparatus |
| CN112151230B (en) * | 2019-06-28 | 2023-05-26 | 西门子(深圳)磁共振有限公司 | Conductive assembly of superconducting magnet and superconducting magnet |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5524441A (en) * | 1993-12-03 | 1996-06-11 | Gec Alsthom Electromecanique Sa | Lead-in module for the supply of a low critical temperature superconducting electric load |
| GB2330194A (en) * | 1997-09-30 | 1999-04-14 | Oxford Magnet Tech | Improvements in or relating to MRI/NMR systems |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3371145A (en) * | 1968-02-27 | Avco Corp | Cryogenic heat exchanger electrical lead | |
| US4080228A (en) * | 1976-12-10 | 1978-03-21 | Currigan Edward B | Aggregate product and method of applying to surfaces |
| US4485266A (en) * | 1982-07-29 | 1984-11-27 | The United States Of America As Represented By The United States Department Of Energy | Termination for a superconducting power transmission line including a horizontal cryogenic bushing |
| US4537803A (en) * | 1984-05-24 | 1985-08-27 | Westinghouse Corp. | Resins containing a low viscosity organopolysiloxane liquid dielectric and a method of insulating a conductor therewith |
| US5040381A (en) * | 1990-04-19 | 1991-08-20 | Prime Computer, Inc. | Apparatus for cooling circuits |
| DE69229262T2 (en) * | 1992-03-16 | 2000-01-20 | Raytheon Co., Lexington | Heat transfer adhesive |
| US5298679A (en) * | 1992-07-01 | 1994-03-29 | Westinghouse Electric Corp. | Current lead for cryostat using composite high temperature superconductors |
| US5484853A (en) * | 1993-07-28 | 1996-01-16 | China Technical Consultants, Inc. | Cryogenic adhesives made from epoxy terminated urethanes |
| US5742217A (en) * | 1995-12-27 | 1998-04-21 | American Superconductor Corporation | High temperature superconductor lead assembly |
| US6376051B1 (en) * | 1999-03-10 | 2002-04-23 | Matsushita Electric Industrial Co., Ltd. | Mounting structure for an electronic component and method for producing the same |
| US6295834B1 (en) * | 1999-06-30 | 2001-10-02 | Medi-Physics, Inc. | NMR polarization monitoring coils, hyperpolarizers with same, and methods for determining the polarization level of accumulated hyperpolarized noble gases during production |
| US6768409B2 (en) * | 2001-08-29 | 2004-07-27 | Matsushita Electric Industrial Co., Ltd. | Magnetic device, method for manufacturing the same, and power supply module equipped with the same |
-
2005
- 2005-02-05 GB GB0502457A patent/GB2422895B/en not_active Expired - Lifetime
-
2006
- 2006-01-27 CN CN2006100043784A patent/CN1816270B/en not_active Expired - Lifetime
- 2006-02-03 US US11/346,342 patent/US20060207266A1/en not_active Abandoned
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5524441A (en) * | 1993-12-03 | 1996-06-11 | Gec Alsthom Electromecanique Sa | Lead-in module for the supply of a low critical temperature superconducting electric load |
| GB2330194A (en) * | 1997-09-30 | 1999-04-14 | Oxford Magnet Tech | Improvements in or relating to MRI/NMR systems |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2456571A (en) * | 2008-01-21 | 2009-07-22 | Siemens Magnet Technology Ltd | Power Supply Coupling System |
| GB2456571B (en) * | 2008-01-21 | 2010-11-17 | Siemens Magnet Technology Ltd | Tomography system with cooled electrically conductive conduits |
| GB2513151A (en) * | 2013-04-17 | 2014-10-22 | Siemens Plc | Improved thermal contact between cryogenic refrigerators and cooled components |
| GB2513151B (en) * | 2013-04-17 | 2015-05-20 | Siemens Plc | Improved thermal contact between cryogenic refrigerators and cooled components |
Also Published As
| Publication number | Publication date |
|---|---|
| GB0502457D0 (en) | 2005-03-16 |
| CN1816270A (en) | 2006-08-09 |
| US20060207266A1 (en) | 2006-09-21 |
| CN1816270B (en) | 2012-05-02 |
| GB2422895B (en) | 2007-08-01 |
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